NSN 5680-01-303-4040
Part Details | STRUCTURAL CELLULAR CORE MATERIAL
5680-01-303-4040 A light durable material having a cellular core of uniform geometric shapes. It is primarily used for, but not limited to, aircraft structure, such as fuselages, control surfaces, compartments, radomes, and the like. For items with a metallic or nonmetallic facing see PANEL, STRUCTURAL, AIRCRAFT.
Alternate Parts: HRP38GF112.2LB 36X96, HRP3/8-GF11-2.2LB 36X96, HRP38GF112.2LB 36X96, HRP3/8-GF11-2.2LB 36X96, 5680-01-303-4040, 01-303-4040, 5680013034040, 013034040
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 56 | JUN 30, 1989 | 01-303-4040 | 20324 ( CORE MATERIAL, CELLULAR, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5680-01-303-4040
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HRP3/8-GF11-2.2LB 36X96 | 04621 | HEXCEL CORP |
| HRP3/8-GF11-2.2LB 36X96 | 6D159 | HEXCEL CORPORATIONDIV CASA GRANDE PLANT |
Technical Data | NSN 5680-01-303-4040
| Characteristic | Specifications |
|---|---|
| BASIC MATERIAL | GLASS CLOTH, RESIN IMPREGNATED |
| COATING MATERIAL | PLASTIC |
| CELL SIZE | 3/8 IN. |
| NOMINAL DENSITY RATING | 2.0 POUNDS PER CUBIC FOOT |
| MAXIMUM DENSITY RATING | 2.2 POUNDS PER CUBIC FOOT |
| MAXIMUM SERVICE TEMP LIMIT | 325.0 DEG FAHRENHEIT |
| DESIGNED RIBBON DIRECTION DIMENSION | 36.000 IN. |
| TRANSVERSE DIRECTION DIMENSION | 96.000IN. |